Question: Under cruising conditions the distributed load acting on the wing of a small airplane has the idealized variation shown in the figure. Calculate the shear

Under cruising conditions the distributed load acting on the wing of a small airplane has the idealized variation shown in the figure.
Calculate the shear force V and bending moment M at the inboard end of the wing.

1600 N/m 900 N/m 1.0 m

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